Airbus A220-100 vs. Douglas DC-7

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Airbus A220-100 versus Douglas DC-7
35.0 m 114 ft 10 in length 34.00 m 111 ft 6 in
11.5 m 37 ft 9 in height 8.38 m 27 ft 6 in
35.1 m 115 ft 2 in wingspan 35.8 m 117 ft 5 in
2 Turbofans (wing mounted) engines 4 x Wright R-3350 Duplex-Cyclone radial engines
21,000–23,000 lb thrust per engine Approximately 3,400 hp per engine
42,000–46,000 lb total thrust Approximately 13,600 hp total
63,100 kg 139,100 lb MTOW 90,718 kg 200,000 lb
6,390 km 3,451 nm range 6,250 km 3,375 nm
871 km/h 541 mph cruise speed 507 km/h 315 mph
Typical seating 2-class 100-120 capacity Up to 105 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.